EP1771713B1 - Balance ring and method for balancing a rotating component - Google Patents

Balance ring and method for balancing a rotating component Download PDF

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Publication number
EP1771713B1
EP1771713B1 EP05763553A EP05763553A EP1771713B1 EP 1771713 B1 EP1771713 B1 EP 1771713B1 EP 05763553 A EP05763553 A EP 05763553A EP 05763553 A EP05763553 A EP 05763553A EP 1771713 B1 EP1771713 B1 EP 1771713B1
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EP
European Patent Office
Prior art keywords
component
annular body
ring
balance ring
retaining ring
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Not-in-force
Application number
EP05763553A
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German (de)
French (fr)
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EP1771713A1 (en
Inventor
Franz Haimer
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Franz Haimer Maschinenbau KG
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Franz Haimer Maschinenbau KG
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Publication of EP1771713A1 publication Critical patent/EP1771713A1/en
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M1/00Testing static or dynamic balance of machines or structures
    • G01M1/30Compensating imbalance
    • G01M1/36Compensating imbalance by adjusting position of masses built-in the body to be tested
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/21Elements
    • Y10T74/211Eccentric
    • Y10T74/2114Adjustable
    • Y10T74/2115Radially

Definitions

  • the invention relates to a balancing ring and a method for balancing a rotating about a rotation axis component, in particular a tool holder or the like.
  • Rotating machine elements such as eg with the drive spindle of a machine tool detachable tool holder for drills, milling cutters or the like, but also other rotating components, such as spindles or shafts, are conventionally balanced by means of balancing rings which are rotatable in pairs axially adjacent to each other concentric to the axis of rotation of the component are stored on this.
  • the two balancing rings have eccentric center of gravity, whose dependent on the relative rotational position of the two balancing rings, resulting unbalance force is adjusted compensating opposite in balancing the component of the unbalance force of the component.
  • By rotating the balancing rings relative to each other the size of the resulting unbalance force of the balancing rings can be changed.
  • By jointly twisting the two balancing rings the direction of action of the resulting unbalance force can be changed.
  • Such a device is eg in WO 94/16852 A disclosed.
  • Such a balancing ring is rotationally symmetrical as a whole, wherein a rotationally symmetrical design is to be understood here and below to mean a shape which, when rotated about the axis of rotational symmetry, can be brought to coincide with itself in angular steps of constant size. Such a shape can be produced very accurately and reproducibly.
  • the balancing ring according to the invention is mounted centrally, but stationary in the circumferential direction of the component.
  • the centric in its basic position to the rotational axis of the component annular body is guided by the Fmmunsgan eleven in the circumferential direction on all sides radially deflectable on the component, wherein the angular position in which the annular body is deflected relative to the component radially and the extent of the radial deflection, the size and direction of the to compensate for a possible imbalance of the component determined unbalance force.
  • three or more adjusting elements are provided, which allow the ring body with the axis of rotation substantially parallel rotational symmetry axis, but to fix the size and direction of selectable eccentricity relative to the component.
  • the guide arrangement primarily ensures that the annular body is guided radially movably on the component with an axis of rotation of the component which is essentially parallel to the rotational symmetry axis. Suitable for this purpose are, for. B. arranged at an axial distance from each other, annular disc-shaped, axially normal to the axis of rotation extending annular disc surfaces, between which the annular body radially displaceable sitting.
  • the annular body is fixed by means of an all-round radially deflectable spring link assembly on the component.
  • This embodiment has the advantage that the annular body can occupy a concentric rest position relative to the rotational axis of the component, from which it can be deflected by means of the adjusting elements against the spring forces of the spring link arrangement.
  • the ring body can automatically assume its centric rest position in this way, in which the imbalance of the component can be determined without this imbalance is distorted by eccentricities of the annular body.
  • the guide arrangement has a bearing on a cylindrical, concentric to the axis of rotation peripheral surface of the component retaining ring, which is connected via the on all sides radially deflectable spring link assembly with the annular body.
  • the rest position may be eccentric to the axis of rotation of the component, since the eccentricity can also be considered in the balancing process.
  • the spring link arrangement arranged along a concentric to the rotational axis of symmetry circle, comprise at least one substantially deflectable in the direction of the rotational axis of symmetry, radially deflectable spring element which - is axially connected - with its one end portion on the retaining ring and with its other end portion with the annular body.
  • a spring link arrangement works on the principle of a parallel link arrangement with elastic links.
  • the spring element may in this case be designed as a concentric, radially elastically deflectable sleeve relative to the rotational symmetry axis.
  • the sleeve may have an annular closed sleeve wall, but it may also be divided in the circumferential direction by a plurality of axially extending slots in radially deflectable spring segments or spring bars. It is understood that the slot width may possibly be greater than the width of these spring segments in the circumferential direction.
  • the spring link arrangement in the circumferential direction of Ring body distributes a plurality of pairs circumferentially extending spring bars, in particular a plurality of pairs of such spring bars comprise, which are held with their circumferentially adjacent ends in pairs on the ring body or in pairs on the retaining ring, and with their circumferentially remote ends of the other component, Retaining ring or ring body - be held.
  • Advantage of the latter spring bars is that they allow comparatively long resilient web lengths, and in the radial displacement of the annular body are able to perform this exactly radially.
  • the spring assembly and the retaining ring may be separately manufactured components, which are subsequently combined to the balancing ring.
  • the ring body, the spring assembly and the retaining ring are integrally formed in one piece, which improves the precision of the balancing ring.
  • the retaining ring may be a closed ring, which is slid and fitted accurately on a corresponding peripheral surface of the component.
  • the retaining ring is attached by heat shrink technology to the component. It is understood that other conventional types of fastening can be used, for example by screwing on the component or by clamping using clamping screws. It is understood that the retaining ring on the component can also be soldered, welded or glued. It is also conceivable to provide the retaining ring with an internal thread, via which it can be screwed to the component.
  • the retaining ring may also be formed as a segmented ring whose segments are connected via the spring arrangement with the annular body.
  • the retaining ring segments may have radial elastic properties, whereby the balancing ring can be held on the component via a radially resilient clamping seat.
  • the actuators may be radially screwed setscrews.
  • the screws can be screwed into a thread of the retaining ring and supported on the ring body.
  • a variant in which the adjusting screws are arranged in screw holes of the annular body and are supported on the retaining ring or directly on the component is easier to produce and easier to adjust.
  • the actuator may be formed as a wedge surface gear in which the wedge either in the circumferential direction, but preferably in the axial direction movable radially displaces the ring body. If the adjusting movement of such an actuating element runs parallel to the axis of rotation, then the adjusting elements do not influence the angular position of the unbalance vector of the annular body.
  • actuators are mechanical transmission elements that allow a change in the support length.
  • the guide arrangement has a retaining ring resting on a cylindrical circumferential surface of the component concentric with the axis of rotation, on which the annular body is supported by a plurality of circumferentially distributed actuator elements having electrically controllable radial support length.
  • Such actuators can be piezoelectric elements or nano-tube elements or the like, which change their spatial dimensions when an electrical voltage or a current is applied.
  • the invention in a second aspect, relates to a method for balancing a rotating about a rotation axis component by means of a attached to the component balancing rings.
  • the method is characterized in that a balancing ring with a radially guided on the component ring body is mounted on the component, which is supported relative to the component via a plurality of circumferentially of the ring body, preferably at equal angular intervals from each other arranged adjusting elements with variable support length, that the component is driven in rotation together with the balancing ring about the rotation axis and a parameter representing the size and direction of the imbalance force occurring here is measured, and that depending on the measured unbalance parameter, the support length of the adjusting elements is changed, such that the ring body in one of the unbalance compensating radial position is shifted.
  • length adjustment information for the control elements is determined here as a function of the measured imbalance parameter. This can be done, for example, that is displayed on a display of the unbalance parameter measuring balancing machine by what value each of the control elements must be changed in its support length to compensate for the imbalance of the component.
  • the display can indicate the number and direction of the revolutions by which each individual adjusting screw is to be turned.
  • a radially adjustable balancing ring 7 is mounted on a circular cylindrical peripheral surface 5 of the component.
  • the balancing ring 7 has an annularly closed retaining ring 9, with which it is held, for example, in shrink fit on the peripheral surface 5, and a radially adjustable balancing mass forming annular body 11, via a spring arm arrangement in the form of a coaxial to the rotation axis 3 radially between the retaining ring 9 and the ring body 11 extending sleeve 13 is connected to the retaining ring 9.
  • the sleeve 13 has substantially an annular closed peripheral wall and is connected at its one end over its entire circumference by means of a radial web 15 with the retaining ring 9 and at its axially opposite end over its entire circumference by means of a radial web 17 with the annular body 11.
  • the sleeve 13 holds the annular body 11 in a concentric to the rotation axis 3 rest position from which the annular body 11 is radially resiliently deflected under radial elastic deformation of the sleeve 13 with substantially parallel to the axis of rotation 3 rotational symmetry axis.
  • the sleeve 13 acts here in the circumferential direction on all sides in the manner of a parallel link arrangement.
  • the unbalance of the component 1 is conventionally measured during rotation on a balancing machine according to size and angular position.
  • the balancing machine determined according to the thus determined unbalance parameter required to compensate for the imbalance size and angular position of the eccentricity of the balancing ring 7 and expediently provides adjustment parameters for the screws 21, for example in the form of helical angle information for each of the screws 21. It is understood that the imbalance parameters not must necessarily be determined starting from the rest position of the ring body 11. Rather, any eccentric position of the annular body 11 is suitable, which then leads to setting values for the adjusting screws 21 which take into account the arbitrary starting position of the annular body 11.
  • the retaining ring 9 is shrunk onto the peripheral surface 5 of the component 1 in the heat shrinking process, so that it is held by press-fit forces on the component 1. It is understood that the retaining ring 9 can also be otherwise attached to the component 1, for example, welded, soldered or glued can be. Also, the retaining ring 9 may be positively secured, for example by means of a thread on its inner circumference or else it may be fixed or screwed by clamping means, such as clamping screws or the like.
  • the retaining ring 9, the sleeve 13 and the ring body 11 are integrally connected integrally with each other and are preferably made of metal.
  • the balancing ring 7 according to the Figures 1 and 2 has three offset by 120 ° to each other angularly offset on the ring body 11 radially screwed screws 21.
  • Die FIGS. 3 and 4 show a variant of a balancing ring 7a, in contrast to the balancing ring 7 of the Figures 1 and 2 four by 90 ° from each other angularly offset screws 21 a radially screwed to its ring body 11a includes.
  • the adjusting screws 21a are also not supported on the retaining ring 9a, but pass through openings 25 of the retaining ring 9a and are based directly on the peripheral surface 5a of the component 1a.
  • FIGS. 5 and 6 show another variant of the basis of the Figures 1 and 2 explained balancing ring 7, the retaining ring 9 is closed in a ring.
  • the retaining ring 9b of the balancing ring 7b of FIGS. 5 and 6 divided by a plurality of slots 27 into segments 29 which bear radially resiliently on the circumference 5b of the component 1b and fix the balancing ring 7b on the component 1b.
  • the slots 27 may be limited to the retaining ring 9b. But you can also in the radial webs 15b and possibly the sleeve 13b and the radial web 17b extend into, as at 31 in FIG. 6 is indicated.
  • the adjusting screws 21 b can also be supported directly on the component 1 b, they are preferably supported on the segments 29 in order to improve the fixation of the balancing ring 7 b on the component 1 b. It is understood that instead of in FIG. 5 shown three screws 21 b and more screws can be present.
  • FIGS. 7 and 8 show the variant of a balancing ring 7c, in which the adjusting elements are designed as electrically controllable actuators 21c, which change their radial dimensions in not shown supply of electrical signals.
  • the actuators 21c are, for example, piezoelectric elements or nano-tube elements or the like.
  • the actuators 21c sit in guide openings on the outer jacket of the retaining ring 9c on the one hand and on the inner surface of the annular body 11c on the other hand and at the same time take over the radial and axial guidance and fixation of the annular body 11c on the retaining ring 9c.
  • the guide openings can, as in the FIGS.
  • the retaining ring 9c can be secured in the manner explained above on the outer circumference 5c of the component 1c.
  • the annular body 11d are connected via a plurality of pairs of circumferentially extending spring bars 13d with the individual segments 9d of a circumferentially divided into a plurality of segments retaining ring.
  • the retaining ring consists in the illustrated embodiment of three segments 9d, which follow each other in the circumferential direction to form gaps 37, wherein in threaded openings 19d of the annular body seated, radially screwed screws 21 d engage through these gaps 37 and are supported directly on the outer periphery 5d of the component 1d.
  • the pairs of spring webs 13d which are formed substantially as circumferentially curved leaf springs, are connected at their ends remote from each other to the circumferential ends of one of the retaining ring segments 9d.
  • the adjacent ends of the spring bars 13 of the pair are connected centrally between circumferentially successive set screws 21 d with the ring body 11 d.
  • the retaining ring segments 9d may be fixed on the component 1d due to their inherent elasticity; but they can also be otherwise secured, for example glued or soldered or screwed.
  • the balancing ring 7e of the FIG. 10 differs from the growth ring 7d the FIG. 9 essentially only in that the retaining ring 9e is formed as a ring-shaped closed retaining ring, which is similar to the variant of the passage for the passage of the screws 21e FIGS. 3 and 4 , with through holes 25e understand, through which the set screws 21 e can be supported directly on the outer periphery 5e of the component 1e.
  • the spring bars 13e are each connected in the circumferential direction on both sides of each screw 21e with the retaining ring 9e.
  • FIG. 11 shown variant of a balancing ring 7f differs from the balancing ring 7d in FIG. 9 only in that the segmented retaining ring forming segments 9f are not connected at their opposite ends with the circumferentially extending spring bars 13f in pairs, but each in its central region between two circumferentially sequential screws 21f.
  • the spring bars 13f of each pair are accordingly connected to the ring body 11f at their circumferentially distal ends.
  • the retaining ring segments 9f form gaps 37f through which the adjusting screws 21f bear directly on the outer circumference 5f of the component 1f.
  • FIG. 12 shows a variant of a balancing ring 7g, in which the retaining ring 9g according to the variant of FIG. 10 is closed annularly, in turn, the set screws 21g pass through through holes 25g and are supported directly on the outer circumference 5g of the component 1g.
  • the balancing ring 7g between two circumferentially successive setscrews 21g arranged in pairs spring bars 13g connected with their adjacent ends to the retaining ring 9g, while the mutually remote ends are axially connected on both sides of the through holes 25g with the ring body 11g.

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Testing Of Balance (AREA)
  • Pivots And Pivotal Connections (AREA)

Abstract

A balance ring for a component (1) rotating about a rotation axis (3), for example a tool holder for a rotating tool or else a machine spindle or the like, is proposed. The balance ring has an annular body (11) which is rotationally symmetrical with respect to an axis of rotational symmetry, a guide arrangement (13) guiding the annular body (11) in a radially movable but axially fixed manner on the component (1) with an axis of rotational symmetry essentially parallel to the rotation axis (3) of the component (1), and a plurality of adjusting elements (21) arranged in the circumferential direction of the annular body (11), preferably at equal angular distances from one another, radially supported between the annular body (11) and the component (1) and having a variable radial supporting length. The guide arrangement may be designed as an axially extending spring link arrangement or else as spring webs extending in the circumferential direction. Instead of the adjusting screws (21), electrically controllable actuators, such as, for example, piezoelectric elements or nanotube elements, may also be provided.

Description

Die Erfindung betrifft einen Wuchtring sowie ein Verfahren zum Auswuchten eines um eine Drehachse rotierenden Bauteils, insbesondere eines Werkzeughalters oder dergleichen.The invention relates to a balancing ring and a method for balancing a rotating about a rotation axis component, in particular a tool holder or the like.

Rotierende Maschinenelemente, wie z.B. mit- der Antriebsspindel einer Werkzeugmaschine kuppelbare Werkzeughalter für Bohrer, Fräser oder dergleichen, aber auch sonstige rotierende Bauteile, wie z.B. Spindeln oder Wellen, werden herkömmlich mit Hilfe von Wuchtringen ausgewuchtet, die paarweise axial nebeneinander konzentrisch zur Drehachse des Bauteils drehbar an diesem gelagert sind. Die beiden Wuchtringe haben exzentrische Massenschwerpunkte, deren von der Relativdrehstellung der beiden Wuchtringe abhängige, resultierende Unwuchtkraft beim Auswuchten des Bauteils der Unwuchtkraft des Bauteils kompensierend entgegengerichtet eingestellt wird. Durch Verdrehen der Wuchtringe relativ zueinander kann die Größe der resultierenden Unwuchtkraft der Wuchtringe verändert werden. Durch gemeinsames Verdrehen der beiden Wuchtringe kann die Wirkungsrichtung der resultierenden Unwuchtkraft verändert werden. Eine solche Vorrichtung ist z.B. in WO 94/16852 A offenbart.Rotating machine elements, such as eg with the drive spindle of a machine tool detachable tool holder for drills, milling cutters or the like, but also other rotating components, such as spindles or shafts, are conventionally balanced by means of balancing rings which are rotatable in pairs axially adjacent to each other concentric to the axis of rotation of the component are stored on this. The two balancing rings have eccentric center of gravity, whose dependent on the relative rotational position of the two balancing rings, resulting unbalance force is adjusted compensating opposite in balancing the component of the unbalance force of the component. By rotating the balancing rings relative to each other, the size of the resulting unbalance force of the balancing rings can be changed. By jointly twisting the two balancing rings, the direction of action of the resulting unbalance force can be changed. Such a device is eg in WO 94/16852 A disclosed.

Herkömmliche Wuchtringpaare setzen exakt bearbeitete Dreh-Führungsflächen voraus und benötigen vergleichsweise großen Bauraum. Demgegenüber ist es Aufgabe der Erfindung, einen justierbaren Wuchtring mit bezogen auf die maximale Unwucht des Wuchtrings verkleinerten Abmessungen zu schaffen.Conventional pairs of balancing sets require precisely machined turning and guiding surfaces and require comparatively large space. In contrast, it is an object of the invention to provide an adjustable balancing ring with respect to the maximum imbalance of the balancing ring reduced dimensions.

Der erfindungsgemäße Wuchtring für ein um eine Drehachse rotierendes Bauteil, insbesondere einen Werkzeughalter oder dergleichen, umfasst:

  • einen bezogen auf eine Rotationssymmetrieachse rotationssymmetrischen Ringkörper,
  • eine den Ringkörper mit zur Drehachse des Bauteils paralleler Rotationssymmetrieachse radial beweglich, jedoch axial fixiert an dem Bauteil führende Führungsanordnung, und
  • mehrere in Umfangsrichtung des Ringkörpers, vorzugsweise in gleichen Winkelabständen voneinander angeordnete, zwischen dem Ringkörper und dem Bauteil radial abgestützte Stellelemente mit veränderbarer radialer Abstützlänge.
The balancing ring according to the invention for a component rotating about an axis of rotation, in particular a tool holder or the like, comprises:
  • one with respect to a rotational symmetry axis rotationally symmetric ring body,
  • a parallel to the annular body with the axis of rotation of the component Rotational axis of symmetry radially movable, but axially fixed to the component leading guide assembly, and
  • several in the circumferential direction of the annular body, preferably arranged at equal angular intervals from each other, radially supported between the annular body and the component control elements with variable radial support length.

Ein solcher Wuchtring ist insgesamt rotationssymmetrisch, wobei unter einer rotationssymmetrischen Gestaltung hier und im Folgenden eine Form verstanden werden soll, die bei Drehung um die Rotationssymmetrieachse in Winkelschritten gleichbleibender Größe jeweils zur Deckung mit sich selbst gebracht werden kann. Eine solche Form läßt sich sehr exakt und reproduzierbar herstellen. Anders als bei herkömmlichen Wuchtringpaaren, die um die Drehachse des Bauteils drehbar an diesem geführt sein müssen, wird der erfindungsgemäße Wuchtring zentrisch, jedoch in Umfangsrichtung stationär an dem Bauteil befestigt. Der in seiner Grundstellung zur Drehachse des Bauteils zentrische Ringkörper ist mittels der Führunsganordnung in Umfangsrichtung allseitig radial auslenkbar an dem Bauteil geführt, wobei die Winkellage, in der der Ringkörper relativ zu dem Bauteil radial ausgelenkt wird und das Ausmaß der radialen Auslenkung die Größe und Richtung der zur Kompensation einer eventuellen Unwucht des Bauteils bestimmten Unwuchtkraft festliegt. In Umfangsrichtung verteilt sind drei oder mehr Stellelemente vorgesehen, die es erlauben, den Ringkörper mit zur Drehachse im Wesentlichen paralleler Rotationssymmetrieachse, jedoch nach Größe und Richtung wählbarer Exzentrizität, relativ zum Bauteil zu fixieren.Such a balancing ring is rotationally symmetrical as a whole, wherein a rotationally symmetrical design is to be understood here and below to mean a shape which, when rotated about the axis of rotational symmetry, can be brought to coincide with itself in angular steps of constant size. Such a shape can be produced very accurately and reproducibly. Unlike conventional balancing-ring pairs, which must be guided rotatably on this about the axis of rotation of the component, the balancing ring according to the invention is mounted centrally, but stationary in the circumferential direction of the component. The centric in its basic position to the rotational axis of the component annular body is guided by the Führunsganordnung in the circumferential direction on all sides radially deflectable on the component, wherein the angular position in which the annular body is deflected relative to the component radially and the extent of the radial deflection, the size and direction of the to compensate for a possible imbalance of the component determined unbalance force. Distributed in the circumferential direction, three or more adjusting elements are provided, which allow the ring body with the axis of rotation substantially parallel rotational symmetry axis, but to fix the size and direction of selectable eccentricity relative to the component.

Die Führungsanordnung sorgt in erster Linie dafür, dass der Ringkörper mit zur Drehachse des Bauteils im Wesentlichen paralleler Rotationssymmetrieachse radial beweglich an dem Bauteil geführt ist. Hierfür geeignet sind z. B. in axialem Abstand voneinander angeordnete, ringscheibenförmige, achsnormal zur Drehachse verlaufende Ringscheibenflächen, zwischen welchen der Ringkörper radial verschiebbar sitzt. Von besonderem Vorteil sind jedoch Ausgestaltungen, bei welchen der Ringkörper mittels einer allseitig radial auslenkbaren Federlenkeranordnung an dem Bauteil fixiert ist. Diese Ausgestaltung hat den Vorteil, dass der Ringkörper eine zur Drehachse des Bauteils konzentrische Ruhelage einnehemen kann, aus der er mittels der Stellelemente gegen die Federkräfte der Federlenkeranordnung ausgelenkt werden kann. Der Ringkörper kann auf diese Weise selbsttätig seine zentrische Ruhelage einnehmen, in der die Unwucht des Bauteils bestimmt werden kann, ohne dass diese Unwucht durch Exzentrizitäten des Ringkörpers verfälscht wird. In einer bevorzugten Ausgestaltung ist vorgesehen, dass die Führungsanordnung einen an einer zylindrischen, zur Drehachse konzentrischen Umfangsfläche des Bauteils anliegenden Haltering aufweist, der über die allseitig radial auslenkbare Federlenkeranordnung mit dem Ringkörper verbunden ist. Die Ruhelage kann jedoch exzentrisch zur Drehachse des Bauteils liegen, da die Exzentrizität auch beim Wuchtvorgang berücksichtigt werden kann.The guide arrangement primarily ensures that the annular body is guided radially movably on the component with an axis of rotation of the component which is essentially parallel to the rotational symmetry axis. Suitable for this purpose are, for. B. arranged at an axial distance from each other, annular disc-shaped, axially normal to the axis of rotation extending annular disc surfaces, between which the annular body radially displaceable sitting. Of particular advantage, however, embodiments in which the annular body is fixed by means of an all-round radially deflectable spring link assembly on the component. This embodiment has the advantage that the annular body can occupy a concentric rest position relative to the rotational axis of the component, from which it can be deflected by means of the adjusting elements against the spring forces of the spring link arrangement. The ring body can automatically assume its centric rest position in this way, in which the imbalance of the component can be determined without this imbalance is distorted by eccentricities of the annular body. In a preferred embodiment, it is provided that the guide arrangement has a bearing on a cylindrical, concentric to the axis of rotation peripheral surface of the component retaining ring, which is connected via the on all sides radially deflectable spring link assembly with the annular body. However, the rest position may be eccentric to the axis of rotation of the component, since the eccentricity can also be considered in the balancing process.

Die Federlenkeranordnung kann, längs eines zur Rotationssymmetrieachse konzentrischen Kreises angeordnet, wenigstens ein im Wesentlichen in Richtung der Rotationssymmetrieachse sich erstreckendes, radial auslenkbares Federelement umfassen, das - axial gesehen - mit seinem einen Endbereich am Haltering und mit seinem anderen Endbereich mit dem Ringkörper verbunden ist. Eine solche Federlenkeranordnung arbeitet nach dem Prinzip einer Parallellenkeranordnung mit elastischen Lenkern. Das Federelement kann hierbei als zur Rotationssymmetrieachse konzentrische, radial elastisch auslenkbare Hülse ausgebildet sein. Die Hülse kann eine ringförmig geschlossene Hülsenwand haben, sie kann aber auch in Umfangsrichtung durch mehrere axial verlaufende Schlitze in radial auslenkbare Federsegmente oder Federstege unterteilt sein. Es versteht sich, dass die Schlitzbreite ggf. auch größer sein kann als die Breite dieser Federsegmente in Umfangsrichtung.The spring link arrangement, arranged along a concentric to the rotational axis of symmetry circle, comprise at least one substantially deflectable in the direction of the rotational axis of symmetry, radially deflectable spring element which - is axially connected - with its one end portion on the retaining ring and with its other end portion with the annular body. Such a spring link arrangement works on the principle of a parallel link arrangement with elastic links. The spring element may in this case be designed as a concentric, radially elastically deflectable sleeve relative to the rotational symmetry axis. The sleeve may have an annular closed sleeve wall, but it may also be divided in the circumferential direction by a plurality of axially extending slots in radially deflectable spring segments or spring bars. It is understood that the slot width may possibly be greater than the width of these spring segments in the circumferential direction.

In einer Variante kann die Federlenkeranordnung in Umfangsrichtung des Ringkörpers verteilt mehrere Paare in Umfangsrichtung sich erstreckender Federstege, insbesondere mehrere Paare solcher Federstege umfassen, die mit ihren in Umfangsrichtung benachbarten Enden paarweise an dem Ringkörper oder paarweise an dem Haltering gehalten sind, und mit ihren in Umfangsrichtung entfernt gelegenen Enden an der jeweils anderen Komponente - Haltering oder Ringkörper - gehalten sein. Vorteil der letztgenannten Federstege ist, dass sie vergleichsweise lange federnde Steglängen ermöglichen, und bei der Radialverschiebung des Ringkörpers in der Lage sind, diesen exakt radial zu führen.In a variant, the spring link arrangement in the circumferential direction of Ring body distributes a plurality of pairs circumferentially extending spring bars, in particular a plurality of pairs of such spring bars comprise, which are held with their circumferentially adjacent ends in pairs on the ring body or in pairs on the retaining ring, and with their circumferentially remote ends of the other component, Retaining ring or ring body - be held. Advantage of the latter spring bars is that they allow comparatively long resilient web lengths, and in the radial displacement of the annular body are able to perform this exactly radially.

Bei dem Ringkörper, der Federanordnung und dem Haltering kann es sich um gesondert hergestellte Bauelemente handeln, die nachträglich zu dem Wuchtring vereinigt werden. In einer bevorzugten Ausgestaltng sind jedoch der Ringkörper, die Federanordnung und der Haltering integral einteilig ausgebildet, was die Präzision des Wuchtrings verbessert.In the annular body, the spring assembly and the retaining ring may be separately manufactured components, which are subsequently combined to the balancing ring. In a preferred embodiment, however, the ring body, the spring assembly and the retaining ring are integrally formed in one piece, which improves the precision of the balancing ring.

Bei dem Haltering kann es sich um einen geschlossenen Ring handeln, der passgenau auf eine entsprechende Umfangsfläche des Bauteils aufgeschoben und befestigt wird. Zweckmäßigerweise wird der Haltering durch Wärmeschrumpftechnik an dem Bauteil befestigt. Es versteht sich, dass auch andere, herkömmliche Befestigungsarten genutzt werden können, beispielsweise durch Anschrauben an dem Bauteil oder durch Anklemmen mittels Klemmschrauben. Es versteht sich, dass der Haltering an dem Bauteils auch angelötet, anschweißt oder angeklebt werden kann. Auch ist denkbar, den Haltering mit einem Innengewinde zu versehen, über das er an dem Bauteil angeschraubt werden kann.The retaining ring may be a closed ring, which is slid and fitted accurately on a corresponding peripheral surface of the component. Conveniently, the retaining ring is attached by heat shrink technology to the component. It is understood that other conventional types of fastening can be used, for example by screwing on the component or by clamping using clamping screws. It is understood that the retaining ring on the component can also be soldered, welded or glued. It is also conceivable to provide the retaining ring with an internal thread, via which it can be screwed to the component.

Der Haltering kann jedoch auch als segmentierter Ring ausgebildet sein, dessen Segmente über die Federanordnung mit dem Ringkörper verbunden sind. Die Halteringsegmente können radialelastische Eigenschaften haben, wodurch der Wuchtring über einen radial federnden Klemmsitz an dem Bauteil gehalten werden kann. Auch hier können jedoch die vorangegangen erläuterten Befestigungsarten eingesetzt werden.However, the retaining ring may also be formed as a segmented ring whose segments are connected via the spring arrangement with the annular body. The retaining ring segments may have radial elastic properties, whereby the balancing ring can be held on the component via a radially resilient clamping seat. Again, however, the above-explained types of attachment can be used.

Bei den Stellelementen kann es sich um radial verschraubbare Stellschrauben handeln. Die Stellschrauben können in ein Gewinde des Halterings geschraubt sein und sich an dem Ringkörper abstützen. Einfacher herstellbar und einfacher einstellbar ist jedoch eine Variante, in der die Stellschrauben in Schraublöchern des Ringkörpers angeordnet sind und sich an dem Haltering oder direkt an dem Bauteil abstützen.The actuators may be radially screwed setscrews. The screws can be screwed into a thread of the retaining ring and supported on the ring body. However, a variant in which the adjusting screws are arranged in screw holes of the annular body and are supported on the retaining ring or directly on the component is easier to produce and easier to adjust.

Es versteht sich, dass anstelle radial beweglicher Stellelemente auch andere den Ringkörper radial auslenkende Stellelemente vorgesehen sein können. Geeignet sind beispielsweise Stellelemente auf der Basis von Schrägflächenführungen oder Lenkerführungen, die eine von der Radialbewegung abweichende Stellbewegung des Lenkerelements zulassen. Beispielsweise kann das Stellelement als Keilflächengetriebe ausgebildet sein, bei welchem der entweder in Umfangsrichtung, vorzugsweise aber in Axialrichtung bewegliche Keil den Ringkörper radial verstellt. Verläuft die Stellbewegung eines solchen Stellelements parallel zur Drehachse, so beeinflussen die Stellelemente die Winkellage des Unwuchtvektors des Ringkörpers nicht.It is understood that, instead of radially movable adjusting elements, it is also possible for other adjusting elements which radially deflect the annular body to be provided. Suitable, for example, adjusting elements on the basis of inclined surface guides or handlebar guides, which allow a deviating from the radial movement adjusting movement of the link element. For example, the actuator may be formed as a wedge surface gear in which the wedge either in the circumferential direction, but preferably in the axial direction movable radially displaces the ring body. If the adjusting movement of such an actuating element runs parallel to the axis of rotation, then the adjusting elements do not influence the angular position of the unbalance vector of the annular body.

Bei den vorstehend erläuterten Stellelementen handelt es sich um mechanische Getriebeelemente, die eine Veränderung der Abstützlänge erlauben. In einer Variante kann vorgesehen sein, dass die Führungsanordung einen an einer zylindrischen, zur Drehachse konzentrischen Umfangsfläche des Bauteils anliegenden Haltering aufweist, an dem der Ringkörper über mehrere in Umfangsrichtung verteilte, die Stellelemente bildende Aktuatoren mit elektrisch steuerbarer radialer Abstützlänge abgestützt ist. Bei solchen Aktuatoren kann es sich um piezoelektrische Elemente oder Nano-Tube-Elemente oder dergleichen handeln, die beim Anlegen einer elektrischen Spannung bzw. eines Stroms ihre räumlichen Abmessungen verändern.In the above-described actuators are mechanical transmission elements that allow a change in the support length. In a variant, it may be provided that the guide arrangement has a retaining ring resting on a cylindrical circumferential surface of the component concentric with the axis of rotation, on which the annular body is supported by a plurality of circumferentially distributed actuator elements having electrically controllable radial support length. Such actuators can be piezoelectric elements or nano-tube elements or the like, which change their spatial dimensions when an electrical voltage or a current is applied.

Unter einem zweiten Aspekt betrifft die Erfindung ein Verfahren zum Auswuchten eines um eine Drehachse rotierenden Bauteils mittels eines an dem Bauteil angebrachten Wuchtrings. Das Verfahren ist dadurch gekennzeichnet, dass an dem Bauteil ein Wuchtring mit einem radial beweglich an dem Bauteil geführten Ringkörper angebracht wird, der über mehrere in Umfangsrichtung des Ringkörpers, vorzugsweise in gleichen Winkelabständen voneinander angeordnete Stellelemente mit veränderbarer Abstützlänge relativ zu dem Bauteil abgestützt ist, dass das Bauteil zusammen mit dem Wuchtring um die Drehachse rotierend angetrieben und ein die Größe und Richtung der hierbei auftretenden Unwuchtkraft repräsentierender Parameter gemessen wird, und dass abhängig von dem gemessenen Unwuchtparameter die Abstützlänge der Stellelemente verändert wird, derart, dass der Ringkörper in eine die Unwuchtkraft kompensierende radiale Position verschoben wird. Zweckmäßigerweise werden hierbei abhängig von dem gemessenen Unwuchtparameter Längeneinstellinformationen für die Stellelemente ermittelt. Dies kann beispielsweise so erfolgen, dass auf einem Display der den Unwuchtparameter messenden Wuchtmaschine angezeigt wird, um welchen Wert jedes der Stellelemente in seiner Abstützlänge verändert werden muss, um die Unwucht des Bauteils zu kompensieren. Soweit Stellschrauben als Stellelemente vorgesehen sind, kann das Display die Zahl und Richtung der Umdrehungen angeben, um die jede einzelne Stellschraube zu drehen ist.In a second aspect, the invention relates to a method for balancing a rotating about a rotation axis component by means of a attached to the component balancing rings. The method is characterized in that a balancing ring with a radially guided on the component ring body is mounted on the component, which is supported relative to the component via a plurality of circumferentially of the ring body, preferably at equal angular intervals from each other arranged adjusting elements with variable support length, that the component is driven in rotation together with the balancing ring about the rotation axis and a parameter representing the size and direction of the imbalance force occurring here is measured, and that depending on the measured unbalance parameter, the support length of the adjusting elements is changed, such that the ring body in one of the unbalance compensating radial position is shifted. Expediently, length adjustment information for the control elements is determined here as a function of the measured imbalance parameter. This can be done, for example, that is displayed on a display of the unbalance parameter measuring balancing machine by what value each of the control elements must be changed in its support length to compensate for the imbalance of the component. As far as adjusting screws are provided as adjusting elements, the display can indicate the number and direction of the revolutions by which each individual adjusting screw is to be turned.

Im Folgenden werden Ausführungsbeispiele der Erfindung anhand einer Zeichnung näher erläutert. Hierbei zeigt:

Fig. 1
eine teilweise aufgebrochene Axialansicht eines Wuchtrings gemäß der Erfindung;
Fig. 2
einen Axiallängsschnitt des Wuchtrings, gesehen entlang einer Linie II-II in Fig. 1;
Fig. 3
eine teilweise aufgebrochene Axialansicht einer ersten Variante des Wuchtrings aus Fig. 1;
Fig. 4
einen Axiallängsschnitt der ersten Variante, gesehen entlang einer Linie IV-IV in Fig. 3;
Fig. 5
eine teilweise aufgebrochene Axialansicht einer zweiten Variante des Wuchtrings aus Fig. 1;
Fig. 6
einen Axiallängsschnitt durch die zweite Variante, gesehen entlang einer Linie VI-VI in Fig. 5;
Fig. 7
eine teilweise aufgebrochene Axialansicht einer zweiten Ausführungsform eines Wuchtrings;
Fig. 8
einen Axiallängsschnitt durch die zweite Ausführungsform, gesehen entlang einer Linie VIII-VIII in Fig. 7;
Fig. 9
eine teilweise aufgebrochene Axialansicht einer dritten Ausführungsform eines Wuchtrings, und
Fig. 10 bis 12
teilweise aufgebrochene Axialansichten von Varianten des Wuchtrings in Fig. 9.
In the following, embodiments of the invention will be explained in more detail with reference to a drawing. Hereby shows:
Fig. 1
a partially broken axial view of a balancing ring according to the invention;
Fig. 2
a Axiallängsschnitt the balancing ring, as seen along a line II-II in Fig. 1 ;
Fig. 3
a partially broken away axial view of a first variant of the balancing ring Fig. 1 ;
Fig. 4
a Axiallängsschnitt the first variant, as seen along a line IV-IV in Fig. 3 ;
Fig. 5
a partially broken axial view of a second Variant of the balancing ring Fig. 1 ;
Fig. 6
a Axiallängsschnitt through the second variant, as seen along a line VI-VI in Fig. 5 ;
Fig. 7
a partially broken away axial view of a second embodiment of a balancing ring;
Fig. 8
an axial longitudinal section through the second embodiment, as seen along a line VIII-VIII in Fig. 7 ;
Fig. 9
a partially broken away axial view of a third embodiment of a balancing ring, and
10 to 12
partially broken axial views of variants of the balancing ring in Fig. 9 ,

Zum Auswuchten eines in den Fig. 1 und 2 allgemein mit 1 bezeichneten, um eine Drehachse 3 rotierenden Bauteils, beispielsweise eines Werkzeughalters, eines Werkzeugs, einer Welle oder einer Arbeitsspindel einer Maschine, ist auf einer kreiszylindrischen Umfangsfläche 5 des Bauteils ein radial einstellbarer Wuchtring 7 befestigt. Der Wuchtring 7 hat einen ringförmig geschlossenen Haltering 9, mit dem er z.B. im Schrumpfsitz auf der Umfangsfläche 5 gehalten ist, sowie einen eine radial verstellbare Wuchtmasse bildenden Ringkörper 11, der über eine Federlenkeranordnung in Form einer koaxial zur Drehachse 3 radial zwischen dem Haltering 9 und dem Ringkörper 11 sich erstreckenden Hülse 13 mit dem Haltering 9 verbunden ist. Die Hülse 13 hat im Wesentlichen eine ringförmig geschlossene Umfangswand und ist an ihrem einen Ende über ihren gesamten Umfang mittels eines Radialstegs 15 mit dem Haltering 9 und an ihrem axial anderen Ende über ihren gesamten Umfang mittels eines Radialstegs 17 mit dem Ringkörper 11 verbunden.To balance one in the Fig. 1 and 2 generally designated 1, about a rotational axis 3 rotating component, such as a tool holder, a tool, a shaft or a work spindle of a machine, a radially adjustable balancing ring 7 is mounted on a circular cylindrical peripheral surface 5 of the component. The balancing ring 7 has an annularly closed retaining ring 9, with which it is held, for example, in shrink fit on the peripheral surface 5, and a radially adjustable balancing mass forming annular body 11, via a spring arm arrangement in the form of a coaxial to the rotation axis 3 radially between the retaining ring 9 and the ring body 11 extending sleeve 13 is connected to the retaining ring 9. The sleeve 13 has substantially an annular closed peripheral wall and is connected at its one end over its entire circumference by means of a radial web 15 with the retaining ring 9 and at its axially opposite end over its entire circumference by means of a radial web 17 with the annular body 11.

Die Hülse 13 hält den Ringkörper 11 in einer zur Drehachse 3 konzentrischen Ruhelage, aus der der Ringkörper 11 unter radialelastischer Verformung der Hülse 13 mit im Wesentlichen zur Drehachse 3 paralleler Rotationssymmetrieachse radial federnd auslenkbar ist. Die Hülse 13 wirkt hierbei in Umfangsrichtung allseitig nach Art einer Parallellenkeranordnung.The sleeve 13 holds the annular body 11 in a concentric to the rotation axis 3 rest position from which the annular body 11 is radially resiliently deflected under radial elastic deformation of the sleeve 13 with substantially parallel to the axis of rotation 3 rotational symmetry axis. The sleeve 13 acts here in the circumferential direction on all sides in the manner of a parallel link arrangement.

In Umfangsrichtung, in gleichen Winkelabständen verteilt, sitzen in Gewindelöchern 19 des Ringkörpers 11 drei von radial außen zugängliche, radial verschraubbare Stellschrauben 21, die die Hülse 13 in Durchgangslöchern 23 durchsetzen und sich am Außenumfang des seinerseits am Bauteil fixierten Halterings 9 abstützen. Durch Verschrauben der Stellschrauben 21 kann der Ringkörper 11 aus seiner zur Drehachse 3 konzentrischen Ruhelage mit zur Drehachse 3 im Wesentlichen paralleler Rotationssymmetrieachse radial in eine exzentrische Lage verstellt werden, wobei die Größe und Winkellage der Exzentrizität durch die Einstellung der drei Stellschrauben 21 wählbar ist. Die Exzentrizität des Ringkörpers 11 wird so gewählt, dass die von dem Ringkörper 11 und ggf. der Hülse 13 erzeugte Unwuchtkraft eine eventuelle Unwucht des Bauteils 1 kompensiert.In the circumferential direction, distributed at equal angular intervals sit in threaded holes 19 of the annular body 11, three radially outwardly accessible, radially screwed set screws 21, which pass through the sleeve 13 in through holes 23 and are supported on the outer periphery of the part fixed to the retaining ring 9. By screwing the screws 21, the annular body 11 can be adjusted from its concentric to the rotation axis 3 rest position with the axis of rotation 3 substantially parallel rotational symmetry axis radially in an eccentric position, the size and angular position of the eccentricity by the setting of the three screws 21 can be selected. The eccentricity of the annular body 11 is selected so that the imbalance force generated by the annular body 11 and possibly the sleeve 13 compensates for any imbalance of the component 1.

Die Unwucht des Bauteils 1 wird herkömmlich bei Rotation auf einer Wuchtmaschine nach Größe und Winkellage gemessen. Die Wuchtmaschine ermittelt entsprechend dem so bestimmten Unwuchtparameter die zum Ausgleich der Unwucht erforderliche Größe und Winkellage der Exzentrizität des Wuchtrings 7 und liefert zweckmäßigerweise Justierparameter für die Stellschrauben 21, beispielsweise in Form von Schraubwinkelinformationen für jede der Stellschrauben 21. Es versteht sich, dass die Unwuchtparameter nicht zwingend ausgehend von der Ruhelage des Ringkörpers 11 bestimmt werden müssen. Geeignet ist vielmehr jede, auch exzentrische Stellung des Ringkörpers 11, die dann zu Einstellwerten für die Stellschrauben 21 führt, die die willkürliche Ausgangsposition des Ringkörpers 11 berücksichtigen.The unbalance of the component 1 is conventionally measured during rotation on a balancing machine according to size and angular position. The balancing machine determined according to the thus determined unbalance parameter required to compensate for the imbalance size and angular position of the eccentricity of the balancing ring 7 and expediently provides adjustment parameters for the screws 21, for example in the form of helical angle information for each of the screws 21. It is understood that the imbalance parameters not must necessarily be determined starting from the rest position of the ring body 11. Rather, any eccentric position of the annular body 11 is suitable, which then leads to setting values for the adjusting screws 21 which take into account the arbitrary starting position of the annular body 11.

Im vorangegangen beschriebenen Ausführungsbeispiel ist der Haltering 9 auf die Umfangsfläche 5 des Bauteils 1 im Wärmeschrumpfverfahren aufgeschrumpft, so dass er durch Presssitzkräfte an dem Bauteil 1 gehalten ist. Es versteht sich, dass der Haltering 9 auch anderweitig an dem Bauteil 1 befestigt sein kann, beispielsweise angeschweißt, angelötet oder angeklebt sein kann. Auch kann der Haltering 9 formschlüssig befestigt sein, beispielsweise mittels eines Gewindes an seinem Innenumfang oder aber er kann durch Klemmmittel, beispielsweise Klemmschrauben oder dergleichen fixiert oder angeschraubt sein.In the embodiment described above, the retaining ring 9 is shrunk onto the peripheral surface 5 of the component 1 in the heat shrinking process, so that it is held by press-fit forces on the component 1. It is understood that the retaining ring 9 can also be otherwise attached to the component 1, for example, welded, soldered or glued can be. Also, the retaining ring 9 may be positively secured, for example by means of a thread on its inner circumference or else it may be fixed or screwed by clamping means, such as clamping screws or the like.

Der Haltering 9, die Hülse 13 und der Ringkörper 11 sind integral einstückig miteinander verbunden und bestehen vorzugsweise aus Metall.The retaining ring 9, the sleeve 13 and the ring body 11 are integrally connected integrally with each other and are preferably made of metal.

Im Folgenden werden Varianten und Ausgestaltungen des Wuchtrings erläutert. Gleich wirkende Komponenten sind jeweils mit vorangegangen erläuterten Bezugszahlen bezeichnet und zur Unterscheidung mit einem Buchstaben versehen. Zur Erläuterung des Aufbaus, der Wirkungsweise und eventueller Varianten wird jeweils auf die vorangegangene Beschreibung Bezug genommen.In the following, variants and configurations of the balancing ring are explained. Equal-acting components are each referred to with previously explained reference numerals and provided for discrimination with a letter. To explain the structure, the mode of action and possible variants, reference is made in each case to the preceding description.

Der Wuchtring 7 gemäß den Figuren 1 und 2 hat drei um 120° gegeneinander winkelversetzt an dem Ringkörper 11 radial verschraubbare Stellschrauben 21. Die Figuren 3 und 4 zeigen eine Variante eines Wuchtrings 7a, der im Unterschied zum Wuchtring 7 der Figuren 1 und 2 vier um jeweils 90° gegeneinander winkelversetzte Stellschrauben 21 a radial verschraubbar an seinem Ringkörper 11a umfasst. Die Stellschrauben 21a stützen sich darüber hinaus nicht an dem Haltering 9a ab, sondern durchsetzen Durchtrittsöffnungen 25 des Halterings 9a und stützen sich direkt an der Umfangsfläche 5a des Bauteils 1a ab.The balancing ring 7 according to the Figures 1 and 2 has three offset by 120 ° to each other angularly offset on the ring body 11 radially screwed screws 21. Die FIGS. 3 and 4 show a variant of a balancing ring 7a, in contrast to the balancing ring 7 of the Figures 1 and 2 four by 90 ° from each other angularly offset screws 21 a radially screwed to its ring body 11a includes. The adjusting screws 21a are also not supported on the retaining ring 9a, but pass through openings 25 of the retaining ring 9a and are based directly on the peripheral surface 5a of the component 1a.

Die Figuren 5 und 6 zeigen eine weitere Variante des anhand der Figuren 1 und 2 erläuterten Wuchtrings 7, dessen Haltering 9 ringförmig geschlossen ist. Im Unterschied dazu ist der Haltering 9b des Wuchtrings 7b der Figuren 5 und 6 durch mehrere Schlitze 27 in Segmente 29 unterteilt, die radial federnd am Umfang 5b des Bauteils 1b anliegen und den Wuchtring 7b an dem Bauteil 1b fixieren. Die Schlitze 27 können auf den Haltering 9b beschränkt sein. Sie können sich aber auch in die Radialstege 15b und ggf. die Hülse 13b und den Radialsteg 17b hinein erstrecken, wie dies bei 31 in Figur 6 angedeutet ist. Wenngleich sich die Stellschrauben 21 b auch direkt am Bauteil 1b abstützen können, so stützen sie sich hier bevorzugt an den Segmenten 29 ab, um die Fixierung des Wuchtrings 7b an dem Bauteil 1b zu verbessern. Es versteht sich, dass anstelle der in Figur 5 dargestellten drei Stellschrauben 21 b auch mehr Stellschrauben vorhanden sein können.The FIGS. 5 and 6 show another variant of the basis of the Figures 1 and 2 explained balancing ring 7, the retaining ring 9 is closed in a ring. In contrast, the retaining ring 9b of the balancing ring 7b of FIGS. 5 and 6 divided by a plurality of slots 27 into segments 29 which bear radially resiliently on the circumference 5b of the component 1b and fix the balancing ring 7b on the component 1b. The slots 27 may be limited to the retaining ring 9b. But you can also in the radial webs 15b and possibly the sleeve 13b and the radial web 17b extend into, as at 31 in FIG. 6 is indicated. Although the adjusting screws 21 b can also be supported directly on the component 1 b, they are preferably supported on the segments 29 in order to improve the fixation of the balancing ring 7 b on the component 1 b. It is understood that instead of in FIG. 5 shown three screws 21 b and more screws can be present.

In den Ausführungsformen der Figuren 1-6 sind die Stellelemente als manuell zu bedienende Stellschrauben ausgebildet. Die Figuren 7 und 8 zeigen die Variante eines Wuchtrings 7c, bei welchem die Stellelemente als elektrisch steuerbare Aktuatoren 21c ausgebildet sind, die bei nicht näher dargestellter Zuführung elektrischer Signale ihre radialen Abmessungen ändern. Bei den Aktuatoren 21c handelt es sich beispielsweise um piezoelektrische Elemente oder Nano-Tube-Elemente oder dergleichen. Die Aktuatoren 21c sitzen in Führungsöffnungen am Außenmantel des Halterings 9c einerseits und am Innenmantel des Ringkörpers 11 c andererseits und übernehmen so zugleich die radiale und axiale Führung und Fixierung des Ringkörpers 11c am Haltering 9c. Die Führungsöffnungen können, wie in den Figuren 7 und 8 dargestellt, als Ringnuten 33 bzw. 35 ausgebildet sein, in welchen die Aktuatoren 21c in jeweils gleichen Winkelabständen voneinander fixiert sind. Es versteht sich, dass elektrisch steuerbare Aktuatoren auch bei den vorangegangen erläuterten und den nachfolgenden Ausführungsbeispielen eingesetzt werden können. Der Haltering 9c kann in der vorangegangen erläuterten Weise am Außenumfang 5c des Bauteils 1c befestigt sein.In the embodiments of the Figures 1-6 the control elements are designed as manually operated screws. The FIGS. 7 and 8 show the variant of a balancing ring 7c, in which the adjusting elements are designed as electrically controllable actuators 21c, which change their radial dimensions in not shown supply of electrical signals. The actuators 21c are, for example, piezoelectric elements or nano-tube elements or the like. The actuators 21c sit in guide openings on the outer jacket of the retaining ring 9c on the one hand and on the inner surface of the annular body 11c on the other hand and at the same time take over the radial and axial guidance and fixation of the annular body 11c on the retaining ring 9c. The guide openings can, as in the FIGS. 7 and 8 illustrated, may be formed as annular grooves 33 and 35, in which the actuators 21c are fixed in each case at equal angular intervals. It is understood that electrically controllable actuators can also be used in the previously explained and the following embodiments. The retaining ring 9c can be secured in the manner explained above on the outer circumference 5c of the component 1c.

Bei den vorangegangen anhand der Figuren 1-6 erläuterten Varianten bestimmt in erster Linie die axiale Länge der die Federlenkeranordnung bildenden Hülse die Federeigenschaften. Die Abmessungen des Wuchtrings in axialer Richtung lassen sich klein halten, wenn, wie in den nachfolgend erläuterten Ausführungsbeispielen, die federnde Länge der Federlenkeranordnung sich nicht in axialer Richtung, sondern in Umfangsrichtung des Ringkörpers erstreckt. In Umfangsrichtung steht vergleichsweise viel Bauraum für die Unterbringung der Federlenkeranordnung zur Verfügung. So zeigt Figur 9 eine Variante eines Wuchtrings 7d, dessen Ringkörper 11d über mehrere Paare von in Umfangsrichtung sich erstreckenden Federstegen 13d mit den einzelnen Segmenten 9d eines in Umfangsrichtung in mehrere Segmente unterteilten Halterings verbunden sind. Der Haltering besteht im dargestellten Ausführungsbeispiel aus drei Segmenten 9d, die in Umfangsrichtung unter Bildung von Lücken 37 aufeinanderfolgen, wobei in Gewindeöffnungen 19d des Ringkörpers sitzende, radial verschraubbare Stellschrauben 21 d durch diese Lücken 37 greifen und sich unmittelbar am Außenumfang 5d des Bauteils 1d abstützen.In the preceding on the basis of Figures 1-6 variants explained determines the spring characteristics in the first place, the axial length of the sleeve forming the spring arm assembly. The dimensions of the balancing ring in the axial direction can be kept small if, as in the embodiments explained below, the resilient length of the spring arm arrangement does not extend in the axial direction but in the circumferential direction of the annular body. In the circumferential direction is comparatively much space for the accommodation of the Spring link arrangement available. So shows FIG. 9 a variant of a balancing ring 7d, the annular body 11d are connected via a plurality of pairs of circumferentially extending spring bars 13d with the individual segments 9d of a circumferentially divided into a plurality of segments retaining ring. The retaining ring consists in the illustrated embodiment of three segments 9d, which follow each other in the circumferential direction to form gaps 37, wherein in threaded openings 19d of the annular body seated, radially screwed screws 21 d engage through these gaps 37 and are supported directly on the outer periphery 5d of the component 1d.

Die Paare der im Wesentlichen als in Umfangsrichtung gekrümmte Blattfedern ausgebildeten Federstege 13d sind mit ihren voneinander entfernten Enden jeweils mit den in Umfangsrichtung gelegenen Enden eines der Halteringsegmente 9d verbunden. Die einander benachbarten Enden der Federstege 13 des Paars sind mittig zwischen in Umfangsrichtung aufeinanderfolgenden Stellschrauben 21 d mit dem Ringkörper 11 d verbunden.The pairs of spring webs 13d, which are formed substantially as circumferentially curved leaf springs, are connected at their ends remote from each other to the circumferential ends of one of the retaining ring segments 9d. The adjacent ends of the spring bars 13 of the pair are connected centrally between circumferentially successive set screws 21 d with the ring body 11 d.

Die Halteringsegmente 9d können auf Grund ihrer Eigenelastizität am Bauteil 1d fixiert sein; sie können aber auch anderweitig befestigt sein, beispielsweise angeklebt oder angelötet oder angeschraubt sein.The retaining ring segments 9d may be fixed on the component 1d due to their inherent elasticity; but they can also be otherwise secured, for example glued or soldered or screwed.

Der Wuchtring 7e der Figur 10 unterscheidet sich vom Wuchtring 7d der Figur 9 im Wesentlichen nur dadurch, dass der Haltering 9e als ringförmig geschlossener Haltering ausgebildet ist, der für den Durchtritt der Stellschrauben 21e, ähnlich der Variante der Figuren 3 und 4, mit Durchgangslöchern 25e verstehen ist, durch die hindurch sich die Stellschrauben 21 e direkt am Außenumfang 5e des Bauteils 1e abstützen können. Die Federstege 13e sind jeweils in Umfangsrichtung beiderseits jeder Stellschraube 21e mit dem Haltering 9e verbunden.The balancing ring 7e of the FIG. 10 differs from the growth ring 7d the FIG. 9 essentially only in that the retaining ring 9e is formed as a ring-shaped closed retaining ring, which is similar to the variant of the passage for the passage of the screws 21e FIGS. 3 and 4 , with through holes 25e understand, through which the set screws 21 e can be supported directly on the outer periphery 5e of the component 1e. The spring bars 13e are each connected in the circumferential direction on both sides of each screw 21e with the retaining ring 9e.

Die in Figur 11 dargestellte Variante eines Wuchtrings 7f unterscheidet sich von dem Wuchtring 7d in Figur 9 lediglich dadurch, dass die einen segmentierten Haltering bildenden Segmente 9f nicht an ihren voneinander abgewandten Enden mit den in Umfangsrichtung sich erstreckenden Federstegen 13f paarweise verbunden sind, sondern jeweils in ihrem Mittelbereich zwischen zwei in Umfangsrichtung aufeinanderfolgenden Stellschrauben 21f. Die Federstege 13f jedes Paars sind dementsprechend an ihren in Umfangsrichtung entfernt gelegenen Enden mit dem Ringkörper 11f verbunden. Auch in der Variante der Figur 11 bilden die Halteringsegmente 9f Lücken 37f, durch die hindurch die Stellschrauben 21f unmittelbar am Außenumfang 5f des Bauteils 1f anliegen.In the FIG. 11 shown variant of a balancing ring 7f differs from the balancing ring 7d in FIG. 9 only in that the segmented retaining ring forming segments 9f are not connected at their opposite ends with the circumferentially extending spring bars 13f in pairs, but each in its central region between two circumferentially sequential screws 21f. The spring bars 13f of each pair are accordingly connected to the ring body 11f at their circumferentially distal ends. Also in the variant of FIG. 11 The retaining ring segments 9f form gaps 37f through which the adjusting screws 21f bear directly on the outer circumference 5f of the component 1f.

Figur 12 zeigt eine Variante eines Wuchtrings 7g, bei welcher der Haltering 9g entsprechend der Variante der Figur 10 ringförmig geschlossen ist, wobei wiederum die Stellschrauben 21g durch Durchgangslöcher 25g treten und sich unmittelbar am Außenumfang 5g des Bauteils 1g abstützen. Im Unterschied zum Wuchtring 7e der Figur 10 sind jedoch bei dem Wuchtring 7g die zwischen zwei in Umfangsrichtung aufeinanderfolgenden Stellschrauben 21g paarweise angeordneten Federstege 13g mit ihren einander benachbarten Enden mit dem Haltering 9g verbunden, während die voneinander entfernt gelegenen Enden axial beiderseits der Durchgangslöcher 25g mit dem Ringkörper 11g verbunden sind. FIG. 12 shows a variant of a balancing ring 7g, in which the retaining ring 9g according to the variant of FIG. 10 is closed annularly, in turn, the set screws 21g pass through through holes 25g and are supported directly on the outer circumference 5g of the component 1g. In contrast to the growth ring 7e the FIG. 10 However, in the balancing ring 7g, between two circumferentially successive setscrews 21g arranged in pairs spring bars 13g connected with their adjacent ends to the retaining ring 9g, while the mutually remote ends are axially connected on both sides of the through holes 25g with the ring body 11g.

Es versteht sich, dass sich die Stellschrauben 21g und 21 e der in den Figuren 10 und 12 dargestellten Wuchtrings auch an dem ringförmig geschlossenen Haltering abstützen können, wie dies für den Wuchtring 7 in den Figuren 1 und 2 erläutert wurde. Die Fixierung der Halteringe an dem Bauteil kann durch Aufschrumpfen, Aufkleben, Aufschweißen erfolgen, wie dies vorangegangen erläutert wurde.It is understood that the screws 21g and 21 e in the FIGS. 10 and 12 shown balancing rings can also be supported on the annular closed retaining ring, as for the balancing ring 7 in the Figures 1 and 2 was explained. The fixing of the retaining rings on the component can be done by shrinking, gluing, welding, as explained above.

Claims (16)

  1. A balance ring for a component (1) rotating about a rotation axis (3), in particular a tool holder or the like, comprising:
    - an annular body (11) which is rotationally symmetrical with respect to an axis of rotational symmetry,
    - a guide arrangement (13, 21c) guiding the annular body (11) on the component (1) in a radially movable but axially fixed manner with an axis of rotational symmetry essentially parallel to the rotation axis (3) of the component (1), and
    - a plurality of adjusting elements (21) arranged in the circumferential direction of the annular body (11), preferably at equal angular distances from one another, radially supported between the annular body and the component and having a variable radial supporting length.
  2. The balance ring as claimed in claim 1, characterized in that the guide arrangement has a retaining ring (9) which bears against a cylindrical circumferential surface, concentric to the rotation axis, of the component (1) and which is connected to the annular body (11) via a spring link arrangement (13) radially deflectable universally.
  3. The balance ring as claimed in claim 2, characterized in that the spring link arrangement (13) is arranged along a circle concentric to the axis of rotational symmetry and comprises at least one radially deflectable spring element (13) which extends essentially in the direction of the axis of rotational symmetry and which - as viewed axially - is connected with its one end region (15) to the retaining ring (9) and with its other end region (17) to the annular body (11).
  4. The balance ring as claimed in claim 3, characterized in that the spring element is an elastically deflectable sleeve (13) concentric to the axis of rotational symmetry.
  5. The balance ring as claimed in claim 4, characterized in that the sleeve (13) is subdivided in the circumferential direction into radially deflectable spring segments by a plurality of axially running slots (27) or apertures.
  6. The balance ring as claimed in claim 2, characterized in that the spring link arrangement, in a distributed manner in the circumferential direction, comprises a plurality of pairs of spring webs (13d-g) which extend in the circumferential direction and which are held with their ends which are adjacent in the circumferential direction in pairs on the annular body (11d-g) or in pairs on the retaining ring (9d-g) and are held with their ends which are remote in the circumferential direction on the other respective component - retaining ring (9d-g) or annular body (11d-g).
  7. The balance ring as claimed in one of claims 2 to 6, characterized in that the annular body (11), the spring arrangement (13) and the retaining ring (9) are integrally formed in one piece.
  8. The balance ring as claimed in one of claims 2 to 7, characterized in that the retaining ring (9, 9a, e, d) is designed as a closed ring.
  9. The balance ring as claimed in claim 8, characterized in that the retaining ring (9) can be shrunk onto the component (1).
  10. The balance ring as claimed in one of claims 2 to 7, characterized in that the retaining ring (9b, d, f) is designed as a segmented ring, the segments of which are connected to the annular body (11b, d, f) via the spring arrangement (13b, d, f).
  11. The balance ring as claimed in one of claims 1 to 10, characterized in that the adjusting elements are designed as adjusting screws (21) which can be screwed down radially.
  12. The balance ring as claimed in claim 11 in combination with one of claims 2 to 10, characterized in that the adjusting screws (21) are arranged in screw holes (19) of the annular body (11) and are supported on the retaining ring or directly on the component.
  13. The balance ring as claimed in claim 1, characterized in that the guide arrangement has a retaining ring (9c) which bears against a cylindrical circumferential surface, concentric to the rotation axis (3), of the component (1c) and on which the annular body (11c) is supported via a plurality of actuators (21c) which are distributed in the circumferential direction, form the adjusting elements and have a controllable radial supporting length.
  14. The balance ring as claimed in claim 13, characterized in that the actuators are designed as piezoelectric elements or nanotube elements.
  15. A method for balancing a component rotating about a rotation axis (3) by means of a balance ring (7) attached to the component, characterized in that a balance ring (7) having an annular body (11) guided on the component (1) in a radially movable manner is attached to the component, which balance ring (7) is supported relative to the component (1) via a plurality of adjusting elements (21) arranged in the circumferential direction of the annular body (11), preferably at equal angular distances from one another, and having a variable supporting length, in that the component (1) together with the balance ring (7) is rotationally driven about the rotation axis (3), and an unbalance parameter representing the size and direction of the unbalance force occurring in the process is measured, and in that the supporting length of the adjusting elements (21) is varied as a function of the measured unbalance parameter in such a way that the annular body (11) is displaced into a radial position compensating for the unbalance force.
  16. The method as claimed in claim 15, characterized in that length-setting information for the adjusting elements (21) is determined as a function of the measured unbalance parameter.
EP05763553A 2004-07-27 2005-07-27 Balance ring and method for balancing a rotating component Not-in-force EP1771713B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102004036394A DE102004036394A1 (en) 2004-07-27 2004-07-27 Balancing ring and method for balancing a rotating component
PCT/EP2005/008152 WO2006010607A1 (en) 2004-07-27 2005-07-27 Balance ring and method for balancing a rotating component

Publications (2)

Publication Number Publication Date
EP1771713A1 EP1771713A1 (en) 2007-04-11
EP1771713B1 true EP1771713B1 (en) 2011-11-30

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Family Applications (1)

Application Number Title Priority Date Filing Date
EP05763553A Not-in-force EP1771713B1 (en) 2004-07-27 2005-07-27 Balance ring and method for balancing a rotating component

Country Status (8)

Country Link
US (1) US7950280B2 (en)
EP (1) EP1771713B1 (en)
JP (1) JP4754564B2 (en)
CN (1) CN100587438C (en)
AT (1) ATE535791T1 (en)
DE (1) DE102004036394A1 (en)
ES (1) ES2375367T3 (en)
WO (1) WO2006010607A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102017108666A1 (en) 2017-04-24 2018-10-25 EZU-Metallwaren GmbH & Co. KG Workpiece adapter for use in a machine tool and workpiece clamping system

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006041417B3 (en) * 2006-09-04 2008-04-03 JOH. WINKLHOFER & SÖHNE GMBH & Co. KG Traction drive with a compensation device for vibration reduction
DE102007025934B4 (en) * 2007-06-04 2015-02-12 Siemens Aktiengesellschaft machine tool
JP2009281462A (en) * 2008-05-21 2009-12-03 Ntn Corp Aerostatic journal bearing spindle
EP2226529B1 (en) * 2009-03-03 2012-06-13 Siemens Aktiengesellschaft An apparatus comprising a shaft and a balancing sleeve
CN102346087A (en) * 2011-06-17 2012-02-08 大连交通大学 Lossless dynamic balance mechanism
DE102012110139A1 (en) 2012-10-24 2014-05-08 Haimer Gmbh Balancing fixture for balancing rotary component e.g. rotating tool or tool receiver, has erosion device that is provided for removing the material at balancing point determined by measuring device and is designed as laser device
CN103115724B (en) * 2013-01-29 2015-05-20 深圳大学 Online dynamic balance compensation device and method for high-speed motorized spindles
US9221141B1 (en) * 2013-02-27 2015-12-29 The Boeing Company Tuned mass tool holder
CN103567809B (en) * 2013-10-16 2016-06-08 杨孝晟 Transient equilibrium structure
CA2945468A1 (en) * 2014-04-14 2015-10-22 Kawasaki Jukogyo Kabushiki Kaisha Toroidal continuously variable transmission
CN105345041B (en) * 2015-11-14 2018-02-16 宁波金凯机床股份有限公司 High-speed main spindle device with autobalance
DE102016117434B4 (en) * 2016-09-15 2018-04-12 Schenck Rotec Gmbh Apparatus and method for attaching a balance weight to a mounting surface on an inner side of a rim
FR3071313B1 (en) * 2017-09-20 2021-01-15 Safran Aircraft Engines REMOVABLE COLLAR TO IDENTIFY AN UNBALANCE OF A ROTARY SHAFT
JP7131305B2 (en) * 2018-11-01 2022-09-06 株式会社Ihi Clamping device and balance measuring device
CN110181423A (en) * 2018-12-25 2019-08-30 海尼肯智能技术成都有限公司 Composite material blade butt clamping ring
CN109470410A (en) * 2019-01-14 2019-03-15 北京航空航天大学 Symmetrical counterweight planetary gear train dynamic balance adjusting apparatus
CN117620324A (en) * 2023-12-21 2024-03-01 杭州新世宝电动转向系统有限公司 Worm gear running-in device of steering gear

Family Cites Families (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US861463A (en) * 1907-01-31 1907-07-30 Oscar H Hyde Balancing emery-wheels and similar devices.
US2241637A (en) * 1938-05-17 1941-05-13 Cincinnati Grinders Inc Dynamic balancing mechanism for machine tools
US2861471A (en) * 1956-08-27 1958-11-25 Leblond Mach Tool Co R K Balancing device
FR2446472A1 (en) * 1978-06-12 1980-08-08 Aerospatiale METHOD AND DEVICE FOR BALANCING PASSIVE AND ACTIVE AXIAL MAGNETIC SUSPENSION ROTATING BODIES AND ORIENTATION OF THEIR ROTATION AXIS
US4253806A (en) * 1979-04-13 1981-03-03 Flo-Tork Inc. Low speed hydraulic motor with counter balanced planetating drive ring and spring biased vanes
JPS6041535Y2 (en) * 1980-02-27 1985-12-18 株式会社リコー Rotating body center of gravity position adjustment device
JPS56126650A (en) * 1980-03-07 1981-10-03 Fuji Heavy Ind Ltd Air-fuel ratio controlling apparatus
SU1037095A1 (en) * 1981-04-02 1983-08-23 Kupryashov Vasilij D Device for balancing shafts
JPS61140343A (en) * 1984-12-12 1986-06-27 Jidosha Kiki Co Ltd Gear rolling apparatus
JPS61140343U (en) * 1985-02-20 1986-08-30
JPS62140343A (en) * 1985-12-13 1987-06-23 Hitachi Ltd Holding device for assembly of deflection yoke
EP0318627A1 (en) * 1987-12-03 1989-06-07 René Linder Device for driving compensation masses of dynamic balancer used by grinders and by other machines
US5074723A (en) * 1989-04-13 1991-12-24 Kennametal Inc. Method and apparatus for balancing a rotary tool assembly
JPH0333003A (en) * 1989-06-28 1991-02-13 Hitachi Ltd Device for forming superconducting thin film
JP2501874Y2 (en) * 1989-08-09 1996-06-19 日本精工株式会社 Spindle device
JPH04201155A (en) * 1990-11-30 1992-07-22 Ariyoshi Kiko Shiyuudan:Kk Balancing device for main spindle of machine tool
JP2638376B2 (en) 1991-02-20 1997-08-06 株式会社東海理化電機製作所 Conductor connection method
US5466049A (en) * 1992-01-27 1995-11-14 Harmsen; Arlyn Balancing ring
JPH0562754U (en) * 1992-02-03 1993-08-20 豊田工機株式会社 Rotary axis balance device
US5263995A (en) 1993-01-27 1993-11-23 Kennametal Inc. Apparatus and method for balancing a rotary tool assembly
JPH06239155A (en) * 1993-02-12 1994-08-30 Suzuki Motor Corp Propeller shaft for automobile
US5555144A (en) * 1995-01-12 1996-09-10 Seagate Technology, Inc. Balancing system for a disc drive disc assembly
JPH1068667A (en) * 1996-08-27 1998-03-10 Mitsubishi Heavy Ind Ltd Automatic rotor balancing device
SE9603105D0 (en) * 1996-08-27 1996-08-27 Skf Ab A method in an autobalancing device
JP3476346B2 (en) * 1997-09-26 2003-12-10 日本電産株式会社 Automatic motor balancing device
CN2368027Y (en) * 1999-03-15 2000-03-08 李启国 Automatic compensation device for dynamic balancing
US6707639B1 (en) * 2000-03-31 2004-03-16 Seagate Technology Llc. Balancing system with adjustable eccentric rings for a disc drive assembly
US6471453B1 (en) * 2001-05-25 2002-10-29 Kennametal Inc. Balancing assembly for a rotating member
DE102006031806A1 (en) * 2006-07-07 2008-01-17 Ewald Chodura Balancing device and method
US7393164B2 (en) * 2006-10-02 2008-07-01 Primetool Mfg, Inc. Dynamic balancing ring for cutter holder

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102017108666A1 (en) 2017-04-24 2018-10-25 EZU-Metallwaren GmbH & Co. KG Workpiece adapter for use in a machine tool and workpiece clamping system
WO2018197022A1 (en) 2017-04-24 2018-11-01 EZU-Metallwaren GmbH & Co. KG Workpiece adapter for use in a machine tool and workpiece clamping system

Also Published As

Publication number Publication date
US20080302181A1 (en) 2008-12-11
EP1771713A1 (en) 2007-04-11
JP4754564B2 (en) 2011-08-24
JP2008508507A (en) 2008-03-21
WO2006010607A1 (en) 2006-02-02
DE102004036394A1 (en) 2006-03-23
ES2375367T3 (en) 2012-02-29
CN100587438C (en) 2010-02-03
CN101023335A (en) 2007-08-22
ATE535791T1 (en) 2011-12-15
US7950280B2 (en) 2011-05-31

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